US2310261A - Pressure responsive device - Google Patents

Pressure responsive device Download PDF

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US2310261A
US2310261A US377034A US37703441A US2310261A US 2310261 A US2310261 A US 2310261A US 377034 A US377034 A US 377034A US 37703441 A US37703441 A US 37703441A US 2310261 A US2310261 A US 2310261A
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chamber
conduit
bore
fluid
housing
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US377034A
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Paul J Schwarzhaupt
Kenneth A Killam
Laurens A Taylor
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General Electric Co
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General Electric Co
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/30Blade pitch-changing mechanisms
    • B64C11/38Blade pitch-changing mechanisms fluid, e.g. hydraulic
    • B64C11/42Blade pitch-changing mechanisms fluid, e.g. hydraulic non-automatic

Definitions

  • the present invention relates to pressure responsive devices, more particularly to differential pressure responsive cutout switches such as rangements include means for adjusting the propeller pitch, that is, the angle between the propeller blade surface and the plane of rotation. Under certain operating conditions, also in case of engine trouble, it is desirable rapidly to feather the propeller, that is, to turn the propeller blades into neutral position in which said angle is about 90.
  • One object of our invention is to provide an improved construction and arrangement of pressure responsive devices, and another object of our invention is to provide an improved differential pressure responsive cutout switch.
  • FIG. 1 illustrates an aircraft propeller feathering arrangement embodying our invention
  • Fig. 2 illustrates a sectional detail view of a differential pressure responsive cutout switch used in the arrangement of Fig. 1
  • Fig. 3 is a section along line 33 of Fig. 2
  • Fig. 2 being a section along line 2-2 of Fig. 3
  • Fig. 4 is an exploded perspective view of a part of Fig. 2.
  • FIG. 1 shows diagrammatically an arrangement for varying the pitch and for feathering of an aircraft propeller.
  • the arrangement comprises a servo motor 2 having a cylinder with a piston 3 movably disposed in the cylinder and definin therewith fluid pressure chambers l and 5.
  • the piston 3 has a stem connected to a sleeve 6 for adjusting the pitch of the blades of a propeller 1.
  • movement of the piston 3 towards the left increases the pitch, and movementof the piston towards the right decreases the pitch.
  • the piston engages a stop 8 and in this position the propeller is feathered, that is, the angle between the propeller blade plane and the plane of rotation is about 90.
  • the hydraulic system for operating the servo motor 2 to vary the propeller pitch and to feather the propeller blades comprises a source 9 of operating fluid, such as oil, and means for forcin the operating fluid from the source to one of the chambers l and and at the same time draining the fluid from the other chamber.
  • a source 9 of operating fluid such as oil
  • the inlet of the .pump I0 is connected to receive operating'fluid from the source 9 and the outlet of the pump H is connected by a conduit 3 to a 3-way valve M.
  • the latter has three ports, a first port connected to the conduit l3, 2. second port connected to one end of a conduit 15 having another end connected to the pressure chamber 4, and a third port connected to one end of a conduit l8 having another end connected to the pressure chamber 5.
  • the arrangement includes a second 3-way valve H which has a first port connected by a conduit Hi to the conduit H, a second port connected by a conduit Hi to the conduit l6, and a third port connected by a conduit 20 to the conduit l5.
  • Both pumps 10 and H are driven from the engine for operating the propeller 1.
  • the pump in may also serve to supply lubricant or operating fluid to bearings and other elements, not shown.
  • the two 3-way valves 14 and il in the present example are connected to and controlled by a speed responsive device shown as a centrifugal type speed governor 2i driven from the engine. ln-the drawing the valves are shown in a neutral position. A change in speed causes turning 02 both 3-way valves H and H by action of the speed governor 2
  • the arrangement includes feathering means to effect rapid feathering of thepropeller whenever desired.
  • This means includes a third positive displacement pump 22 having an inlet conduit 23 connected to the conduit
  • the feathering pump 22 is driven by an electric motor 25 connected to an electric circuit which includes a source of electric energy indicated as a battery 26, a push button 21, and a differential pressure responsive cutout switch 28.
  • the switch 28 is connected by a pipe
  • the displacement of fluid between the chambers 4 and 5 is effected primarily through a bypass formed by a bore 29a through the piston 3.
  • increase in fluid pressure in the chamber 4 forces the piston towards the right with the fluid contained in the chamber 5 displaced and forced into the chamber 4 through the bore 29a in the piston 5.
  • the piston reaches its right-hand end position, engaging the stop 8, the pressure in the chamber 4 is built up further and as it reaches a certain value relative .to the pressure in the other chamber 5 the switch 28' is actuated to disconnect the motor 25 from the source of electric energy 26.
  • the differential pressure responsive cutout switch 28, as shown in Figs. 2, 3, and 4, com prises a housing or receptacle 30 which forms a chamber 3
  • the left-hand end of the housing forms a threaded, tubular extension 34 accommodating two terminals 35 and 36 supported v on and electrically insulated from the housing by insulating material 31.
  • the inner ends of the terminals are screwed into supports 38 and 39 for contacts 40 and 4
  • which preferably are made from silver are integrally united with the metallic supports 38, 39.
  • the contact supports 38, 33 are insulated from the bottom of the housing by a plate 42 of insulating material and from the side wall of the housing by a sheet 43 of e1ectrical insulating material.
  • and the terminals 35, 36 secured thereto are connected to the push button 24 and the motor 22, as shown in Fig. 1.
  • the bottom of the housing 30 is formed with two bores, a centrally located large bore 44 connected to the pipe
  • a piston or plunger 46 is slidably located in the large bore 44.
  • An intermediate portion 4' of the plunger 46 has a larger diameter than the lower portion, thus forming a shoulder 48 and preventing the plunger 45 from dropping out of the chamber 3
  • the upper portion of the plunger 46 is provided with an extension 49 of electrical insulating material. This extension forms a spherically-shaped head engaging a contact-making and breaking disk or like member 50.
  • the disk 50 in the present example is bimetallic, the upper portion consisting of copper and the lower portion or coating consisting of silver to assure a good electrical connection between the contacts 40, 4
  • the cutout switch is simple in design and may be manufactured at comparatively low cost.
  • the contact-making and breaking member due to its spherical engagement with the head 49 and the depression in the spring plate 52, is self-aligning, that is, once the contact-making member is forced down into engagement with the contacts 40, 4
  • the lower end of the central bore 44 according to our invention is connected to the high pressure pipe
  • the chamber 3! is initially filled with operating fiuid such as oil from the low Pressure line We. Due to the fact that the central bore 44 is connected to the high pressure line and some leakage takes place along the clearance between the bore 4d and the plunger 48 into the chamber 3i, ,8, continuous slight leakage circulation from the bore 44 through the chamber 3
  • operating fiuid such as oil from the low Pressure line We. Due to the fact that the central bore 44 is connected to the high pressure line and some leakage takes place along the clearance between the bore 4d and the plunger 48 into the chamber 3i, ,8, continuous slight leakage circulation from the bore 44 through the chamber 3
  • the switch is normally held in closed position, as shown in Figs. 1 and 2.
  • the pipe l5a, and the bore 44 builds up and a predetermined pressure difierenc-e between the pipes i5a and liia is reached, plunger 46 is forced upward and thereby removes the contactmaking member 50 from the contacts 40, 4
  • Pressure responsive device comprising a housing having a bore for connection to a source of fluid under pressure, a plunger slidably prolecting into the bore and having an upper spherical end portion, a member with a central spherical depression loosely and rockingly engaging the spherical end portion, means biasing the member towards the end portion comprising a spring and a'spring plate engaging the spring and having a central depression in engagement with the central portion of the member, and means controlled in response to movement of said member.
  • a differential pressure responsive device comprising a housing forming a chamber and two bores connected to the chamber, a plunger slidably disposed in one of the bores and having a spherical end portion located in the chamber, an actuating member having a central portion with a depression rockingly engaging the spherical end portion of the plunger, means biasing the member towards the plunger comprising a compres sion spring and a spring plate having a central recess rockingly engaging the central portion of said member, and means controlled in response to movemenioi the member.
  • Pressure responsive switch comprising a housing forming a chamber and a bore for connection to a source of fluid under pressure, a plunger movably disposed in the bore and having a spherical end portion of electrical insulating material disposed within the chamber, a contactmaking disk having a central depression loosely and rockingly engaging the spherical end portion, means including a spring and a spring plate made from insulating material for biasing the contact disk towards the spherical end portion, and means including contacts located in the chamber and insulated from the housing in cooperative relation with the contact-making disk.
  • Differential pressure responsive switch comprising a housing forming a pressure chamber, a high pressure bore and a. low pressure bore communicating with the chamber, a plunger sildably projecting into the high pressure bore and having a spherical end portion located in the chamber, a contact-making disk having a central depression rockingly engaging the spherical end portion, electric contacts located in the chamber and electrically insulated from the housing, and spring means for biasing the contact disk towards the spherical head into engagement with the contacts.
  • Differential pressure responsive switch comprising a housing forming a pressure chamber, a bore for connection to a source of high pressure and a bore for connection with a source of low pressure and communicating with the chamher, a. plunger slidably projecting into the high pressure bore and having a spherical end portion made of electrical insulating material located in the chamber, a disk having a central portion with a lower surface concave-shaped and in rocking engagement with said end portion, the central portion of the disk having an upper surface convex-shaped, means biasing the disk towards the plunger comprising a spring and a spring plate having a central portion with a depression rockingly engaging said convex-shaped upper surface of the disk, contacts fastened within and electrically insulated from the housing in cooperative relation with the disk, and terminals projecting through the housing and secured to the contacts.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Switches Operated By Changes In Physical Conditions (AREA)

Description

Feb. 9, 1943. P. J. SCHWARZHAUPT ETAL 2,310,261
PRESSURE RESPONSIVE DEVICE Filed Feb. 1, 1941 v J3 37 V 7 2 5'3 '5 l J! INSULATION Inventors:
T PaulJSchwarzhauQvb,
0 Kenneth A.Kil|am,
Laurens Affaglor, A
9 Then" Attorneg.
Patented Feb. 9, 1943 PRESSURE RESPONSIVE DEVICE Paul J. Schwarzhaupt, Scotia, and Kenneth A. Kill-am and Laurens A. Taylor, Schenectady, N. Y., assignors to General Electric Company, a corporation of New York Application February 1, 1941, Serial No. 377,034
6 Claims.
The present invention relates to pressure responsive devices, more particularly to differential pressure responsive cutout switches such as rangements include means for adjusting the propeller pitch, that is, the angle between the propeller blade surface and the plane of rotation. Under certain operating conditions, also in case of engine trouble, it is desirable rapidly to feather the propeller, that is, to turn the propeller blades into neutral position in which said angle is about 90.
One object of our invention is to provide an improved construction and arrangement of pressure responsive devices, and another object of our invention is to provide an improved differential pressure responsive cutout switch.
For a consideration of what we believe to be novel and our invention, attention is directed to the following description and the claims appended theretoin connection with the accompanying drawing.
In the drawing, Fig. 1 illustrates an aircraft propeller feathering arrangement embodying our invention; Fig. 2 illustrates a sectional detail view of a differential pressure responsive cutout switch used in the arrangement of Fig. 1; Fig. 3 is a section along line 33 of Fig. 2, Fig. 2 being a section along line 2-2 of Fig. 3; and Fig. 4 is an exploded perspective view of a part of Fig. 2.
-Fig. 1 shows diagrammatically an arrangement for varying the pitch and for feathering of an aircraft propeller. The arrangement comprises a servo motor 2 having a cylinder with a piston 3 movably disposed in the cylinder and definin therewith fluid pressure chambers l and 5. The piston 3 has a stem connected to a sleeve 6 for adjusting the pitch of the blades of a propeller 1. During operation, movement of the piston 3 towards the left increases the pitch, and movementof the piston towards the right decreases the pitch. In the right-hand end position the piston engages a stop 8 and in this position the propeller is feathered, that is, the angle between the propeller blade plane and the plane of rotation is about 90.
The hydraulic system for operating the servo motor 2 to vary the propeller pitch and to feather the propeller blades comprises a source 9 of operating fluid, such as oil, and means for forcin the operating fluid from the source to one of the chambers l and and at the same time draining the fluid from the other chamber. In
the present example we have shown two positive displacement pumps I0 and II connected in series by a conduit l2. The inlet of the .pump I0 is connected to receive operating'fluid from the source 9 and the outlet of the pump H is connected by a conduit 3 to a 3-way valve M. The latter has three ports, a first port connected to the conduit l3, 2. second port connected to one end of a conduit 15 having another end connected to the pressure chamber 4, and a third port connected to one end of a conduit l8 having another end connected to the pressure chamber 5. The arrangement includes a second 3-way valve H which has a first port connected by a conduit Hi to the conduit H, a second port connected by a conduit Hi to the conduit l6, and a third port connected by a conduit 20 to the conduit l5.
Both pumps 10 and H are driven from the engine for operating the propeller 1. The pump in may also serve to supply lubricant or operating fluid to bearings and other elements, not shown. The two 3-way valves 14 and il in the present example are connected to and controlled by a speed responsive device shown as a centrifugal type speed governor 2i driven from the engine. ln-the drawing the valves are shown in a neutral position. A change in speed causes turning 02 both 3-way valves H and H by action of the speed governor 2|. If these valves are turned clockwise, the valve H establishes connection between the conduits l3 and i6, whereas the valve ll establishes connection between the conduits l8 and 20. In this position of the valves fluid under pressure is forced through the conduit l3, the valve ll, and the conduit 16 into the chamber 5 and at the same time operating fluid is drained from the chamber 4 through the conduits I5, 20, the valv H, the conduit 18 to the conduit l2, that is, the inlet of the pump II. This causes movement of the piston 3 toward the left, thus changing the propeller pitch. Upon counterclockwise movement of the valves H, il due to a change in speed, the valve l4 connects conduit l3 with conduit I5 and the valve I1 connects conduit 18 with conduit [9. Fluid thus is forced by the pump ll through the conduit i3, the valve I4, and the conduit l5 into the chamber 4. Simultaneously fluid is drained from the chamber 5 through the conduit t6, the conduit IS, the valve I1, and the conduit l8 to the inlet conduit l2 of the pump II. This causes movement of the piston 3 towards the right, thus reducing the propeller pitch. As the piston 3 reaches its end position in which it engages the stop 8, the propeller is feathered, that is, the blades are in neutral position. Broadly the pump eifects displacement of fluid between the chambers 4 and 5, receiving fluid from one chamber and forcing the fluid into the other chamber.
The arrangement includes feathering means to effect rapid feathering of thepropeller whenever desired. This means includes a third positive displacement pump 22 having an inlet conduit 23 connected to the conduit |3, that is, ,to the discharge of the pump II and an outlet conduit 24 connected .to the aforementioned conduit |5. The feathering pump 22 is driven by an electric motor 25 connected to an electric circuit which includes a source of electric energy indicated as a battery 26, a push button 21, anda differential pressure responsive cutout switch 28. The switch 28 is connected by a pipe |a .to the conduit I5 and by a pipe |6a to the conduit l6 and, as will be more fully explained hereinafter, the switch is responsive to the difference between the fluid pressures in said pipes l5 and I6. As this pressure difference increases and reaches a predetermined value the switch automatically opens the circuit for the motor 25.
During operation, closing of the push button 2] starts the motor 25, driving the feathering pump 22. Fluid is then forced through the pumps H), II and the feathering pump 24 into the conduit |5 to the chamber 4. Simultaneously fluid is drained from the chamber 5 through the conduit IS, the valve i4, the conduit I3, to the conduit 23 and the inlet of the feathering pump, the 3-way valve l4 being in position to connect the conduits Hi and I6. Thus, the feathering pump 22 causes displacement of fluid between the chambers 4 and 5, fluid being drained from the chamber 5 and forced through the feathering pump 22 into the chamber 4. The conduit I5 includes a nonreturn valve 29 to prevent return flow of fluid discharged from the feathering pump 22. In case the valves 4 and I1 should for some reason not be in the proper position during feathering operation, the displacement of fluid between the chambers 4 and 5 is effected primarily through a bypass formed by a bore 29a through the piston 3. During operation, increase in fluid pressure in the chamber 4 forces the piston towards the right with the fluid contained in the chamber 5 displaced and forced into the chamber 4 through the bore 29a in the piston 5. As the piston reaches its right-hand end position, engaging the stop 8, the pressure in the chamber 4 is built up further and as it reaches a certain value relative .to the pressure in the other chamber 5 the switch 28' is actuated to disconnect the motor 25 from the source of electric energy 26. a
The differential pressure responsive cutout switch 28, as shown in Figs. 2, 3, and 4, com= prises a housing or receptacle 30 which forms a chamber 3| closed at its upper end by a plug 32 screwed into the housing and sealed thereto by a gasket 33. The left-hand end of the housing forms a threaded, tubular extension 34 accommodating two terminals 35 and 36 supported v on and electrically insulated from the housing by insulating material 31. The inner ends of the terminals are screwed into supports 38 and 39 for contacts 40 and 4| respectively. The contacts 40, 4| which preferably are made from silver are integrally united with the metallic supports 38, 39. The contact supports 38, 33 are insulated from the bottom of the housing by a plate 42 of insulating material and from the side wall of the housing by a sheet 43 of e1ectrical insulating material. The contacts 40, 4| and the terminals 35, 36 secured thereto are connected to the push button 24 and the motor 22, as shown in Fig. 1. The bottom of the housing 30 is formed with two bores, a centrally located large bore 44 connected to the pipe |5a (Fig. l) and another small bore 45 near the side wall of the housing connected to the pipe I611. Both bores 44 and 45 extend .through the bottom to the chamber 3|. A piston or plunger 46 is slidably located in the large bore 44. An intermediate portion 4' of the plunger 46 has a larger diameter than the lower portion, thus forming a shoulder 48 and preventing the plunger 45 from dropping out of the chamber 3|. The upper portion of the plunger 46 is provided with an extension 49 of electrical insulating material. This extension forms a spherically-shaped head engaging a contact-making and breaking disk or like member 50. The disk 50 in the present example is bimetallic, the upper portion consisting of copper and the lower portion or coating consisting of silver to assure a good electrical connection between the contacts 40, 4|.
The central portion 5| of the disk 50 forms a depression. The lower or concave-shaped surface of the central portion 5| engages rockingly the spherical end portion or head 48 of the plunger 46 and the upper or convex-shaped surface of the central portion 5| engages rockingly a spring plate 52 which latter has a central, substantially spherically-shaped relatively small depression 53 in contact with the central portion 5| of the contact-making member 50. The spring plate 52 is biased downward by a compression spring 54 having a lower end located in a recess 55'of the spring plate. The spring 54 is located in an annular recess 56 formed in the plug 32. The compression of -,the spring 54 may be varied by the insertion or the removal of shims 51 in the upper end of the annular recess 56.
During assembly the insulating elements 37, 42 and 43 are inserted and secured to the housing whereupon the contact supports 33, 39 with the contacts 40, 4| are placed into the chamber 3| and secured to the terminals 35, 3B. The plunger 46 with the insulating head 49 is inserted through the chamber into the bore 44. There after the contact-making and breaking disk 5|! is placed on top of the insulating head 49 and .the gasket 33 is placed on the upper end face of the housing. Finally, the plug 32 is assembled with the spring 54 and the spring plate 52 and screwed into the upper end of the housing.
The cutout switch is simple in design and may be manufactured at comparatively low cost. The contact-making and breaking member, due to its spherical engagement with the head 49 and the depression in the spring plate 52, is self-aligning, that is, once the contact-making member is forced down into engagement with the contacts 40, 4|, it will align itself automatically with the contact surface of the contacts 40, 4| and it will remain in this aligned position during subsequent movement of the plunger 46. The lower end of the central bore 44 according to our invention is connected to the high pressure pipe |5a, whereas the small bore 45 at its lower end communicates with an annular groove 58 formed in the lower surface of the housing 30 and connected to the low pressure pipe iSa.
After the switch is installed and put into operation, the chamber 3! is initially filled with operating fiuid such as oil from the low Pressure line We. Due to the fact that the central bore 44 is connected to the high pressure line and some leakage takes place along the clearance between the bore 4d and the plunger 48 into the chamber 3i, ,8, continuous slight leakage circulation from the bore 44 through the chamber 3| and out of the bore 45 into the pipe 16a takes place during operation. This is important because the small clearance between the plunger 46 and the bore 44 prevents solid impurities, that is, large particles that may be contained in the operating fluid from entering the pressure chamber 3!. Thus, the arrangement reduces to a great extent formation of deposits and the accumultaion of solids in the pressure chamber 3|.
As stated before, the switch is normally held in closed position, as shown in Figs. 1 and 2. During -operation, as the pressure in the conduit 24, the pipe l5a, and the bore 44 builds up and a predetermined pressure difierenc-e between the pipes i5a and liia is reached, plunger 46 is forced upward and thereby removes the contactmaking member 50 from the contacts 40, 4|, thus interrupting the electric circuit of the motor 25.
Having described the method of operation of our invention, together wtih the apparatus which we now consider to represent the best embodiment thereof, we desire to have it understood that the apparatus shown is only illustrative and that the invention may be carried out by other means.
What we claim as new and desire to secure by Letters Patent of the United States, is:
1. Pressure responsive device comprising a housing having a bore for connection to a source of fluid under pressure, a plunger slidably prolecting into the bore and having an upper spherical end portion, a member with a central spherical depression loosely and rockingly engaging the spherical end portion, means biasing the member towards the end portion comprising a spring and a'spring plate engaging the spring and having a central depression in engagement with the central portion of the member, and means controlled in response to movement of said member.
2. A differential pressure responsive device comprising a housing forming a chamber and two bores connected to the chamber, a plunger slidably disposed in one of the bores and having a spherical end portion located in the chamber, an actuating member having a central portion with a depression rockingly engaging the spherical end portion of the plunger, means biasing the member towards the plunger comprising a compres sion spring and a spring plate having a central recess rockingly engaging the central portion of said member, and means controlled in response to movemenioi the member.
3. Pressure responsive switch comprising a housing forming a chamber-and a bore, a plunger slidably projecting into the bore and having a spherical end portion of electrical insulating material located in the chamber, a metallic disk having a central portion with a depression loosely and rockingly engaging said spherical end portion, means loosely engaging and biasing the disk towards the spherical end portion, and contact means supported on the housing in cooperative relation with the disk.
4. Pressure responsive switch comprising a housing forming a chamber and a bore for connection to a source of fluid under pressure, a plunger movably disposed in the bore and having a spherical end portion of electrical insulating material disposed within the chamber, a contactmaking disk having a central depression loosely and rockingly engaging the spherical end portion, means including a spring and a spring plate made from insulating material for biasing the contact disk towards the spherical end portion, and means including contacts located in the chamber and insulated from the housing in cooperative relation with the contact-making disk.
5. Differential pressure responsive switch comprising a housing forming a pressure chamber, a high pressure bore and a. low pressure bore communicating with the chamber, a plunger sildably projecting into the high pressure bore and having a spherical end portion located in the chamber, a contact-making disk having a central depression rockingly engaging the spherical end portion, electric contacts located in the chamber and electrically insulated from the housing, and spring means for biasing the contact disk towards the spherical head into engagement with the contacts.
6. Differential pressure responsive switch comprising a housing forming a pressure chamber, a bore for connection to a source of high pressure and a bore for connection with a source of low pressure and communicating with the chamher, a. plunger slidably projecting into the high pressure bore and having a spherical end portion made of electrical insulating material located in the chamber, a disk having a central portion with a lower surface concave-shaped and in rocking engagement with said end portion, the central portion of the disk having an upper surface convex-shaped, means biasing the disk towards the plunger comprising a spring and a spring plate having a central portion with a depression rockingly engaging said convex-shaped upper surface of the disk, contacts fastened within and electrically insulated from the housing in cooperative relation with the disk, and terminals projecting through the housing and secured to the contacts.
PAUL J. SCHWARZHAUPT. KENNETH A. KILLAM. LAURENS A. TAYLOR.
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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426007A (en) * 1942-11-14 1947-08-19 Fairey Aviat Co Ltd Variable pitch propeller arrangement
US2501660A (en) * 1947-08-12 1950-03-28 Wallace R Bohle Fluid pressure switch
US2513660A (en) * 1946-10-22 1950-07-04 United Aircraft Corp Propeller pitch control means
US2533035A (en) * 1947-06-10 1950-12-05 Louis H Morin Pneumatic safety stop for die closures
US2540753A (en) * 1945-03-03 1951-02-06 Westinghouse Air Brake Co Combination valve and switch mechanism
US2545684A (en) * 1945-10-25 1951-03-20 Gen Motors Corp Propeller pitch governor
US2602517A (en) * 1948-01-20 1952-07-08 Glenn L Martin Co Propeller feathering control switch
US2604561A (en) * 1948-11-22 1952-07-22 Joseph M Simon Pressure differential switch
US2719997A (en) * 1952-07-11 1955-10-11 Ackerman Dolletta May Dispenser and applicator
US4005401A (en) * 1974-05-22 1977-01-25 Toyota Jidosha Kogyo Kabushiki Kaisha Electrical switch for a braking fluid pressure fault alarm device

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2426007A (en) * 1942-11-14 1947-08-19 Fairey Aviat Co Ltd Variable pitch propeller arrangement
US2540753A (en) * 1945-03-03 1951-02-06 Westinghouse Air Brake Co Combination valve and switch mechanism
US2545684A (en) * 1945-10-25 1951-03-20 Gen Motors Corp Propeller pitch governor
US2513660A (en) * 1946-10-22 1950-07-04 United Aircraft Corp Propeller pitch control means
US2533035A (en) * 1947-06-10 1950-12-05 Louis H Morin Pneumatic safety stop for die closures
US2501660A (en) * 1947-08-12 1950-03-28 Wallace R Bohle Fluid pressure switch
US2602517A (en) * 1948-01-20 1952-07-08 Glenn L Martin Co Propeller feathering control switch
US2604561A (en) * 1948-11-22 1952-07-22 Joseph M Simon Pressure differential switch
US2719997A (en) * 1952-07-11 1955-10-11 Ackerman Dolletta May Dispenser and applicator
US4005401A (en) * 1974-05-22 1977-01-25 Toyota Jidosha Kogyo Kabushiki Kaisha Electrical switch for a braking fluid pressure fault alarm device

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